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GA_missile_trajectory_simulation
- 提出了一种空面导弹下滑段、俯冲攻击段的弹道优化设计方案,以及一 种实现航向动态跟踪的具体方法。大量算例表明,采用本文中的空面导弹控制 方案可以设计、调试出较满意的弹道,达到获取导弹飞行性能数据并验证导弹总 体设计参数的目的。 -A decline in air-surface missile paragraph, paragraph ballistic dive attack to optimize the design of programs, as well as a cou
MissileTest
- 用户可以使用键盘对飞机进行控制，如导弹的俯仰，偏航，加速等操作，观看的导弹变化飞行目标，爆炸，弹片飞散等尽可能阵势的描述-Users can use the keyboard to control the aircraft, such as the missile' s pitch, yaw and speed up operations, etc. to watch the flight of the changes in the target missile, explosion, s
BTT-missile-flight-envelope-large-multi-mode-metho
- 大包络飞行BTT导弹多模鲁棒控制BTT missile flight envelope large multi-mode method of robust control-BTT missile flight envelope large multi-mode method of robust control
Integgn
- 基于测发一体化技术的导弹发射控制系统设计Integration technology based on measurements made missile launch control system design-Integration technology based on measurements made missile launch control system design
Crme
- 飞航自动驾驶仪系统控制方案研究Cruise Missile Autopilot System Control Scheme-Cruise Missile Autopilot System Control Scheme
zhanluedaodan
- 主要接受战略导弹的测试发射控制方法的发展和相关模拟器在测试发射控制总的运用-Mainly by the strategic missile test launch control simulator in the development and testing related to the use of the total emission control
VSCS
- 自己发表的小论文《导弹变结构控制系统设计》附带程序-His essay published in " missile variable structure control system design" with the program
Missile
- 导弹内部控制系统的设计。包括导弹制导，导弹飞行，导弹控制，通信传输等等部分。-Missile internal control system design. Including missile guidance, missile flight, missile control, communications, transport and so on parts.
IEE-autopilot1
- In this paper, a missile longitudinal autopilot is designed using a new nonlinear control synthesis technique
BTT-missile
- 针对不确定非线性 BTT 导弹控制系统, 提出了一种基于模糊高斯基函数神经网络的自适应控制设计方法。在设计过程中将不确定部分合为一项, 应用模糊神经网络的万能逼近性质来逼近系统不确定项, 然后利用滑模控制和自适应模糊神经网络理论设计了控制器, 应用 Ly apunov 稳定性理论保证闭环系统的稳定性,并推导出自适应律,最后通过仿真结果验证该方法的有效性。-BTT missile based on fuzzy neural network adaptive control
MISSILE
- 针对三点法三维运动学弹道仿真问题，建立了两种仿真模型 第一种模型采用数值积分算法求解 三点法运动学方程组，求解过程较为复杂 第二种模型利用三维空间相关几何知识，将求解三点法三维运动学 弹道的图解法转化为求解一元二次方程的问题，使求解过程简单直观 最后，对两种模型进行了仿真，并将其 应用到地空导弹制导控制系统的仿真研究中，将理想弹道与控制弹道进行了对比 结果表明，两个模型均解决了一般情形下三点法三维运动学弹道求解的问题，为三点法三维制导律以及弹道特性研究提供了一种方法-Three-po
missile
- In this paper, formation control ideas for multiple spacecraft using the virtual structure approach are presented. If there is no formation feedback from the spacecraft to the virtual structure, the spacecraft will get out of formation when the v
coorsinat
- The success of a guided missile is dependent on certain factors. The most significant error sources affecting the success of a guided missile are the initial heading error of the missile and the target maneuvers. Apart from these, the dynamic
aiopng
- 导弹追踪,数学建模，求解导弹轨迹优化控制问题，考虑空气阻力和地球曲率的影响(Missile tracking is used to solve the problem of trajectory optimization control, considering the influence of air resistance and earth curvature and rotation.)